Research Article
PySCP: A Multiple-Phase Optimal Control Software Using Sequential Convex Programming
Table 3
Data of Falcon 9 full thrust rocket.
| | Stage | First | Second |
| | Dry mass (t) | 22.2 | 4.0 | | Propellant mass (t) | 410.9 | 107.5 | | Vacuum thrust (kN) | 8227 | 934 | | Specific impulse (s) | 300 | 350 | | Nozzle exit area (m2) | 11.039 | N/A |
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